Carbon Fiber Fabric Repair Prepreg, 125Mdc (250Mdf) Vacuum Curing Part 0 - Introduction
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Product Code: AMS3970
Date Published: 1999-12-01 - A newer version of this standard is available.
Issuing Committee:
Ams Cacrc Commercial Aircraft Composite Repair Committee
Scope
AMS 3970 gives information about qualification rules and the relation between the different specification parts involved, such as the Technical Specification (TS), Material Specification (MS), and Purchasing Specification (PS). The link to the material qualification and qualified products is presented. This specification is only applicable to carbon fiber fabric and epoxy or modified epoxy resin prepreg systems used for repair of carbon fiber composite structures. Generally, an epoxy or modified epoxy resin film adhesive will be part of the prepreg system for co-cure bonding applications.
Product Status: In Stock
File Size:
36K
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| Current & Historical versions of this standard |
|---|
| Standard |
Date published |
?Status |
| AMS3970A |
2011-04-01 |
Revised |
| AMS3970 |
1999-12-01 |
Issued |
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